Aerodynamic diffuser, contraction, and fairing for disk base and re-acceleration drag reduction in hard disk drives

ABSTRACT

A device streamlines air flow inside a hard disk drive with a stationary afterbody that is located adjacent to the disks. The device gradually expands the air flow so that the speed of the air flow gradually decreases while pressure increases. This design reduces losses in system momentum due to sudden expansion of the air in the drive. In addition, air flow moving toward the disk pack may be contracted to allow efficient energy conversion from pressure energy to kinetic energy prior to merging of the bypass air flow with the air flow among the disks. The device has a comb-like structure that is offset slightly from the spinning disk pack in the radial direction. The structure fulfills an aerodynamic function, reduces track misregistration, lowers overall aerodynamic dissipation and fulfills a filtration function.

BACKGROUND OF THE INVENTION

1. Technical Field

The present invention relates in general to an improved aerodynamicdesign for a diffuser and/or contraction and, in particular, to animproved system, method, and apparatus for diffusing and contracting airflow, especially within a hard disk drive to reduce flow-inducedvibrations of the arm, suspension, and slider as well as the rotatingdisks.

2. Description of the Related Art

Generally, a data access and storage system consists of one or morestorage devices that store data on magnetic or optical storage media.For example, a magnetic storage device is known as a direct accessstorage device (DASD) or a hard disk drive (HDD) and includes one ormore disks and a disk controller to manage local operations concerningthe disks. The hard disks themselves are usually made of aluminum alloyor a mixture of glass and ceramic, and are covered with a magneticcoating. Typically, one to six disks are stacked on a common spindlethat is turned by a disk drive motor at several thousand revolutions perminute (rpm).

A typical HDD also utilizes an actuator assembly. The actuator movesmagnetic read/write heads to the desired location on the rotating diskso as to write information to or read data from that location. Withinmost HDDs, the magnetic read/write head is mounted on a slider. A slidergenerally serves to mechanically support the head and any electricalconnections between the head and the rest of the disk drive system. Thesurface of the slider facing the disk is aerodynamically shaped tocreate an air bearing in order to maintain a uniform distance from thesurface of the rotating disk, thereby preventing the head fromundesirably contacting the disk.

Typically, a slider is formed with an aerodynamic pattern of protrusionson its air bearing surface (ABS) that enables the slider to fly at asubstantially constant height close to the disk during operation of thedisk drive. A slider is associated with each side of each disk and fliesjust over the disk's surface. Each slider is mounted on a suspension toform a head gimbal assembly (HGA). The HGA is then attached to asemi-rigid actuator arm that supports the entire head flying unit.Several semi-rigid arms may be combined to form a single movable unithaving either a linear bearing or a rotary pivotal bearing system.

The head and arm assembly is linearly or pivotally moved utilizing amagnet/coil structure that is often called a voice coil motor (VCM). Thestator of a VCM is mounted to a base plate or casting on which thespindle is also mounted. The base casting with its spindle, actuatorVCM, and internal filtration system is then enclosed with a cover andseal assembly to ensure that no contaminants can enter and adverselyaffect the reliability of the slider flying over the disk. When currentis fed to the motor, the VCM develops a torque that is substantiallyproportional to the applied current. The arm acceleration is thereforesubstantially proportional to the magnitude of the current. As theread/write head approaches a desired track, a reverse polarity signal isapplied to the actuator, causing the signal to act as a brake, andideally causing the read/write head to stop and settle directly over thedesired track.

In the prior art, a number of solutions have been proposed to enhancethe air flow within hard disk drives, such as bypass channels locatedadjacent to the disk pack. For example, Japanese Patent JP53-47089, toYasuaki, reveals a hard disk device in which air guides 20, 30 onlyguide a central portion of the flow of air back to the disks. JapanesePatent JP62-85997, to Wakatsuki, discloses a magnetic disk device (FIGS.3-5) in which a housing 31 with doors 20 guides the flow of air from thedisks to a filter. U.S. Pat. No. 5,907,453, to Wood, reveals diverterramps 220, 222 (FIG. 9) that also only affect a central portion of theair flow.

Currently known implementations of bypass channels such as these force asudden widening of the air flow cross-section by as much as 50%. The sumof the thicknesses of the disk(s) in the disk pack is a significantfraction of the height of the bypass channel in the direction of thespindle axis. As a result, present designs cause objectionable disk basedrag due to the disk wakes in the bypass channel. Moreover, there isalso objectionable drag due to re-acceleration of the slow, bypass airflow around the actuator. Thus, an improved solution for streamliningair flow within a hard disk drive would be desirable.

SUMMARY OF THE INVENTION

One embodiment of an apparatus for streamlining air flow inside of ahard disk drive is disclosed. The air flow is guided into a bypasschannel. Each disk is provided with a stationary afterbody. Theafterbody is shaped such that an expanding duct is created for the flowcoming off each disk. An expanding aerodynamic duct is called adiffuser. In one embodiment, a diffuser provides a gradually expandingpassage so that the speed of the air flow can gradually, rather thanabruptly, decrease and the pressure can rise. This design reduces lossesin system momentum due to sudden expansion of the air or gas in thedrive.

The present invention also ensures a smooth recovery process of pressurefrom kinetic energy in the entering flow field, which reduces the amountof power required by the spindle motor. The downstream diffuser receivesair flow spun off the disks while reducing the rate of cross sectionalexpansion, and consequential turbulence, of the air as it travels fromamong the disk surfaces around the actuator and non-aerodynamic diskdrive components. Upon return of the bypass flow to the disk pack, airflow reentering the disk pack is accelerated in a channel of diminishingcross section to allow efficient energy conversion from pressure energyto kinetic energy prior to merging of the bypass air flow with the airflow among the disks.

The present invention utilizes a comb-like structure (diffuser orcontraction) that is offset slightly from the spinning disk pack in theradial direction by approximately 0.5 mm, or whatever minimal distanceis required due to mechanical tolerances. In one embodiment, thestructure fulfills an aerodynamic function only. However, the structuremay also be configured to perform a filtration function, in which casethe structure may be formed from a filtration substance. The efficacy ofthe filtration material may be enhanced, for example, by incorporationof electric charges (electret). The structure may be provided withlinear or rounded tapers. However, smooth, edge-free tapers aredesirable. For example, since the contraction is required tore-accelerate the air flow into the disk pack, the leading edges of thecontraction are preferably rounded.

The foregoing and other objects and advantages of the present inventionwill be apparent to those skilled in the art, in view of the followingdetailed description of the preferred embodiment of the presentinvention, taken in conjunction with the appended claims and theaccompanying drawings.

BRIEF DESCRIPTION OF THE DRAWINGS

So that the manner in which the features and advantages of theinvention, as well as others which will become apparent are attained andcan be understood in more detail, more particular description of theinvention briefly summarized above may be had by reference to theembodiment thereof which is illustrated in the appended drawings, whichdrawings form a part of this specification. It is to be noted, however,that the drawings illustrate only an embodiment of the invention andtherefore are not to be considered limiting of its scope as theinvention may admit to other equally effective embodiments.

FIG. 1 is a schematic, top plan view of a hard disk drive constructed inaccordance with the present invention.

FIG. 2 is a front isometric view of a diffuser for the hard disk driveof FIG. 1 and is constructed in accordance with the present invention.

FIG. 3 is a rear isometric view of the diffuser of FIG. 2, and isconstructed in accordance with the present invention.

FIG. 4 is a front isometric view of the diffuser of FIG. 2 showing oneof the adjacent disks, and is constructed in accordance with the presentinvention.

FIG. 5 is a front isometric view of a contraction for the hard diskdrive of FIG. 1 and is constructed in accordance with the presentinvention.

FIG. 6 is a rear isometric view of the contraction of FIG. 5, and isconstructed in accordance with the present invention.

DETAILED DESCRIPTION OF THE INVENTION

Referring to FIG. 1, a schematic drawing of one embodiment of aninformation storage system comprising a magnetic hard disk file or drive111 for a computer system is shown. Drive 111 has an outer housing orbase 113 containing a disk pack having at least one media or magneticdisk 115. The disk or disks 115 are rotated (see arrows 205) by aspindle motor assembly having a central drive hub 117. An actuator 121comprises a plurality of parallel actuator arms 125 (one shown) in theform of a comb that is movably or pivotally mounted to base 113 about apivot assembly 123. A controller 119 is also mounted to base 113 forselectively moving the comb of arms 125 relative to disk 115.

In the embodiment shown, each arm 125 has extending from it at least onecantilevered load beam and suspension 127. A magnetic read/writetransducer or head is mounted on a slider 129 and secured to a flexurethat is flexibly mounted to each suspension 127. The read/write headsmagnetically read data from and/or magnetically write data to disk 115.The level of integration called the head gimbal assembly is head and theslider 129, which are mounted on suspension 127. The slider 129 isusually bonded to the end of suspension 127. The head is typically picosize (approximately 1250×1000×300 microns) and formed from ceramic orintermetallic materials. The head also may be of “femto” size(approximately 850×700×230 microns) and is pre-loaded against thesurface of disk 115 (in the range two to ten grams) by suspension 127.

Suspensions 127 have a spring-like quality, which biases or urges theair bearing surface of the slider 129 against the disk 115 to cause theslider 129 to fly at a precise distance from the disk. A voice coil 133free to move within a conventional voice coil motor magnet assembly 134(top pole not shown) is also mounted to arms 125 opposite the headgimbal assemblies. Movement of the actuator 121 (indicated by arrow 135)by controller 119 moves the head gimbal assemblies along radial arcsacross tracks on the disk 115 until the heads settle on their respectivetarget tracks. The head gimbal assemblies operate in a conventionalmanner and always move in unison with one another, unless drive 111 usesmultiple independent actuators (not shown) wherein the arms can moveindependently of one another.

Referring now to FIGS. 1 and 4, the disk pack and disks 115 (one shown)define an axis 201 of rotation 205 and radial directions 207, 209,relative to the axis 201. The disk pack and disks 115 have a downstreamside 213 wherein air flows away from the disks 115, and an upstream side215 wherein air flows toward the disks 115. The drive 111 also has abypass channel 219 formed in the housing 113 for directing the air flowgenerated by rotation of the disks 115 from the downstream side 213 ofthe disk pack or disks 115 to the upstream side 215 of the disk pack ordisks 115. In the embodiment shown, the bypass channel 219 is locatedbetween an outer perimeter 217 (FIG. 1) of the housing 113 and theactuator 121, such that the bypass channel 219 completely circumscribesthe actuator 121. In some HDD designs where there is not sufficientspace to implement a full bypass channel (shown) the bypass channel 219may be interrupted (not shown). This is known as a partial bypass. Whenthere is a partial bypass, the presence of a diffuser and contractionremains beneficial. Furthermore, in order to help the bypass flownegotiate substantial angular changes (channel bends), one or moreturning vanes may be placed in those areas. The use of turning vanes iswell known in wind tunnel design.

As shown in FIGS. 1 through 4, one embodiment of the drive 111constructed in accordance with the present invention also comprises adiffuser 221. In the embodiment shown, the diffuser 221 is located inthe bypass channel 219 and is positioned adjacent to the downstream side213 of the disk pack or disks 115. The diffuser 221 is also offsetdownstream from the disks 115 in the radial direction 207, such that thediffuser 221 reduces air flow drag from the disks 115 due to disk wakein the bypass channel 219. This type of aerodynamic drag is commonlycalled base drag.

Alternatively, or operating in conjunction with the diffuser 221,another embodiment of the drive 111 may include a contraction device orcontraction 223 (FIGS. 5 and 6). The contraction 223 is also located inthe bypass channel 219, but is adjacent to the upstream side 215 of thedisk pack or disks 115. Like the diffuser 221, the contraction 223 isoffset upstream from the disks 115, but in a radial direction 209. Eachof the diffuser 221 and the contraction 223 may be spaced apart fromouter edges 213, 215, respectively, of the disks 115 in radialdirections 207, 209, respectively, by, for example, no more thanapproximately 0.5 mm. The contraction 223 is provided forre-accelerating a slow bypass air flow 225 (FIGS. 1, 5, and 6) from thecontraction 223 to the disks 115 to provide efficient energy conversionfor the air flow from pressure energy to kinetic energy prior to mergingthe slow bypass air flow 225 with air flow 205 (FIG. 1) around the disks115.

In another embodiment of the present invention, each of the diffuser 221and/or the contraction 223 may further comprise an air filter(s) forfiltering the air flowing through the bypass channel 219 and/or housing113. Either or both structures 221, 223 may be configured to performthis filtration function, in which case they may be formed from afiltration substance. In one particular embodiment, the diffuser 221 andthe contraction 223 incorporate electrical charges to filter the airflowing through the bypass channel 219 and/or housing 113. The efficacyof the filtration material may be enhanced, for example, byincorporation of electric charges (electret).

In the embodiments illustrated, both the diffuser 221 and thecontraction 223 are equipped with a plurality of airfoils 231, 233,respectively. The airfoils 231, 233 may be identical but, as shown inthe illustrations, they may be configured differently as well. Theairfoils 231, 233 are axially apart from each other, respectively, inthe axial direction. Each of the airfoils 231, 233 has a generallyplanar orientation in the radial direction. As shown, for example, inFIG. 4, the airfoils 231 (only one shown for clarity) are axiallyaligned with one of the disks 115. The airfoils 231, 233 also having amaximum axial thickness 235 (FIG. 2) that is preferably equal to anaxial thickness 237 (FIG. 4) of a respective one of the disks 115. Thediffuser shape must be such as to promote adherence of the flow to thesurface while avoiding flow separation. It is well known in the art thatflow separation occurs when the diffuser widens too suddenly.Furthermore, it will be understood that an array of flow conditioningmeasures can be applied to the basic diffuser shape shown for thepurpose of promoting adherence of the flow to the diffuser walls. Amongthese measures are turbulators consisting of surface roughness elements,for example ridges, vortex generators, boundary layer tripping devicesand the like. Other flow conditioning measure is irradiation of the flowwith sound. The mentioned flow conditioning techniques are known in theart of aerodynamic design.

Each of the airfoils 231 of the diffuser 221 has a leading edge 241 witha generally cylindrical transverse surface 243 extending in the axialdirection that flatly faces the disks 115. Transverse surface 243 islocated immediately adjacent to a respective one of the disks 115 (seeFIGS. 1 and 4) and is substantially perpendicular to a planarorientation of a respective one of the disks 115. Each of the airfoils233 of the contraction 223 has a trailing edge 251 located immediatelyadjacent to a respective one of the disks 115, and a leading edge 253with a rounded surface 255 that is located opposite the trailing edge251.

The leading edges 241 of the airfoils 231 of the diffuser 221 and thetrailing edges 251 of the airfoils 233 of the contraction 223 havearcuate contours that are complementary in shape with respect tocircular outer edges 213, 215 of the disks 115. The airfoils 231 of thediffuser 221 also have trailing portions 245 located opposite theleading edges 241. The trailing portions 245 taper down in axialthickness in the air flow direction away from the disks 115 to definegradually expanding passages 249. The air flow transitions from thedisks 115 to the trailing portions 245 along the tapers to graduallydecrease a speed of the air flow.

As shown in FIGS. 2-4, the tapers on the airfoils 231 of the diffuser221 are smooth and edge-free from the leading edges 241 to the trailingportions 245. Alternatively, the tapers may be configured with lineartapers. The airfoils 233 of the contraction 223 may be provided withsimilar smooth and edge-free tapers extending from their respectiveleading edges 253 to their respective trailing edges 251. In addition,the trailing portions 245 of the airfoils 231 of the diffuser 221 andthe leading edges 253 of the airfoils 233 of the contraction 223 havelinear edges that are substantially perpendicular to the directions ofthe air flow at the downstream and upstream sides 213, 215,respectively, of the disk pack or disks 115. Furthermore, the leadingedges 253 of the airfoils 233 of the contraction 223 are preferablyrounded 255, as shown in FIGS. 5 and 6.

The present invention has several advantages, including the ability tostreamline air flow in a hard disk drive. The air flow is smoothed intothe bypass channel with a stationary afterbody. The diffuser provides agradual expanding passage so that the speed of the air flow cangradually decrease and the pressure can rise. This design reduces lossesin system momentum due to sudden expansion of the air or gas in thedrive, and ensures a smooth recovery of pressure from kinetic energy inthe entering flow field. As a result, the amount of power required bythe spindle motor is reduced. Alternatively, air flow moving toward thedisk pack is contracted to allow efficient energy conversion frompressure energy to kinetic energy prior to merging of the bypass airflow with the air flow among the disks. The structure also may be usedto filter the air flow. It will be understood that the present inventionencompasses designs in which the diffuser or contraction are notimplemented. The usual reason being interference with other drivecomponents.

While the invention has been shown or described in only some of itsforms, it should be apparent to those skilled in the art that it is notso limited, but is susceptible to various changes without departing fromthe scope of the invention.

1. An apparatus, comprising: a diffuser adapted to reduce drag from adisk due to disk wake in a bypass channel, the diffuser having acomb-like structure having a pair of axially-oriented side walls and atleast one air foil extending between the side walls.
 2. The apparatus ofclaim 1, wherein the diffuser further comprises an air filter forfiltering air flow.
 3. The apparatus of claim 2, wherein the air filterof the diffuser incorporates electrical charges to filter air flow. 4.The apparatus of claim 1, wherein the diffuser has an air foil having agenerally planar orientation.
 5. The apparatus of claim 4, wherein theair foil has a leading edge with a flat transverse surface extending inan axial direction.
 6. The apparatus of claim 5, wherein the leadingedge of the air foil has an arcuate contour.
 7. The apparatus of claim6, wherein the air foil has a trailing portion located opposite theleading edge, and wherein the trailing portion tapers down in axialthickness in an air flow direction to define a gradually expandingpassage, such that the taper gradually decreases a speed of the airflow.
 8. The apparatus of claim 7, wherein the trailing portion of theair foil has a linear trailing edge.
 9. An apparatus, comprising: adiffuser adapted to reduce air flow drag from disks due to disk wake ina bypass channel; a contraction adapted to re-accelerate a slow bypassair flow from the contraction to the disks to provide efficient energyconversion for the air flow from pressure energy to kinetic energy priorto merging the slow bypass air flow with air flow around the disks; andboth the diffuser and the contraction have a plurality of airfoils thatare axially apart from each other, respectively, in an axial direction,each of the airfoils having a generally planar orientation in a radialdirection and being axially aligned with the disks, the airfoils alsohaving a maximum axial thickness that is adapted to be less than orequal to an axial thickness of the disks.
 10. The apparatus of claim 9,wherein each of the diffuser and the contraction further comprise an airfilter for filtering the air flow.
 11. The apparatus of claim 10,wherein the diffuser and the contraction incorporate electrical chargesto filter the air flow.
 12. The apparatus of claim 9, wherein each ofthe airfoils of the diffuser has a leading edge with a flat transversesurface extending in the axial direction, and wherein each of theairfoils of the contraction has a trailing edge and a leading edge witha rounded surface that is located opposite the trailing edge.
 13. Theapparatus of claim 12, wherein the leading edges of the airfoils of thediffuser and the trailing edges of the airfoils of the contraction havearcuate contours.
 14. The apparatus of claim 12, wherein the airfoils ofthe diffuser have trailing portions located opposite the leading edges,and wherein the trailing portions taper down in axial thickness in anair flow direction to define gradually expanding passages, such that asthe air flow transitions from the disks to the trailing portions, thetapers gradually decrease a speed of the air flow.
 15. The apparatus ofclaim 14, wherein the tapers on the airfoils of the diffuser are smoothand edge-free from the leading edges to the trailing portions, andwherein the airfoils of the contraction have similar smooth andedge-free tapers extending from their respective leading edges to theirrespective trailing edges.
 16. The apparatus of claim 14, wherein thetrailing portions of the airfoils of the diffuser and the leading edgesof the airfoils of the contraction have linear edges that aresubstantially perpendicular to the directions of the air flow at thedownstream and upstream sides, respectively, of the disks, and whereinthe leading edges of the airfoils of the contraction are rounded.